N707EV

Service difficulty reports · 227

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N707EV' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR TRAX200800635Seat Track · corrodedCABIN FLOOR SEAT RAILS HAVE CORROSION DAMAGE AT LBL9 FS 379.00 TO FS 477.40. BLENDED CORROSION ON LBL 9 FS 349 TO FS 477.40 REMOVED .020" OF DAMAGE WITHIN LIMITS ALLOWED .035" OF REMOVAL. ALL WORK DONE IAW SRM 53-21-49. DK 7022603 JOB COMPLETE.May 14, 2008 · N707EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR TRAX200800629Web · corrodedRT 280 WEB CORRODED. OPEN (B)May 14, 2008 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200800628Web · corrodedLT 280 WED CORRODED---[OPEN] (B)May 14, 2008 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200800627Floorbeam · corroded280 SUPPORT BEAM CORRODED. REMOVED AND REPLACED STA 280 SUPPORT BEAM PN CC670-34175-7 AS PER SRM 51-42-21, 51-42-06. REO 670-53-11-047, AND SB 670BA-53-026.May 14, 2008 · N707EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR TRAX200800616Drag Angle · crackedVERTICAL STAB LOWER LT DRAG ANGLE IS CRACKED CUT AWAY DAMAGE FROM VERTICAL STAB LOWER LT DRAG ANGLE IAW REO 670-53-31-018. INSTALLED DOBLER AND FILLER, FILLET SEAL REPAIR PARTS AND FINAL PAINT AND LT DRAG ANGLE. ALL WORK DONE IAW REO 670-53-31-018. (B)May 10, 2008 · N707EV · Cndair CL6002C10 · Vertical StabilizerSDR TRAX200800617Drag Angle · crackedVERTICAL STAB LOWER RT DRAG ANGLE IS CRACKED. PERFORMED EDDY CURRENT INSPECTION OF RIGHT V/STAB TO FUSELAGE DRAG ANGLE TO LOCATE END OF CRACK IAW NDTM 51-20-006 END OF CRACK IS MARKED. CUT AWAY DAMAGE FROM VERTICAL STAB LOWER RT DRAG ANGLE IAW REO 670-55-31-May 10, 2008 · N707EV · Cndair CL6002C10 · Vertical StabilizerSDR TRAX200800615Placard · wornPAX DOOR EXIT PLACARD WORN. REPLACED EXIT PLACARD PER AMM 11-30-02.May 10, 2008 · N707EV · Cndair CL6002C10 · Placards and MarkingsSDR TRAX200701078Warning System · activatedAFT CARGO DOOR INDICATES OPEN IN FLIGHT. AFT CARGO DOOR AMBER CAUTION MSG ILLUMINATED. A/C RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED.Jul 29, 2007 · N707EV · Cndair CL6002C10 · Door Warning SystemSDR TRAX200701023Flashlight · inoperativeF/A FLASHLIGHT INOP.Jul 18, 2007 · N707EV · Cndair CL6002C10 · Emergency EquipmentSDR TRAX200700802Light · inoperativeAFT MOST CEILING EMERGENCY LIGHT INOP.Jun 7, 2007 · N707EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200700288Floor Support · corrodedFS 280 FWD CENTER FLOOR SUPPORT ANGLE CORRODED. REMOVED FS 280 FWD CENTER FLOOR SUPPORT ANGLE MH715 LOCATED HOLES IN SERVICEABLE ANGLE P/N CC670-33292-13 IAW CRJ SRM 51-40-11 MH715. OK TO INSTALL. INSTALLED FWD CENTER FLOOR SUPPORT IAW CRJ CRM 51-42-06 & 51Feb 23, 2007 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200700287Crossbeam · corrodedFS 280 CROSSBEAM HAS CORROSION ON UPPER FLANGE. REPLACE BEAM PER CUSTOMER. REMOVED ALL REQUIRED FASTENERS ON LEFT FS 280. CROSSBEAM, REMOVED LBL 9 CLIP, REMOVED LEFT FS 280 CROSSBEAM. ALL WORK DONE IAW CRJ SRM 51-42-06, 51-42-13, 51-42-21. LOCATED HOLES OFeb 23, 2007 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200700290Web · corrodedRT LOWER FS 280 WEB HAS CORROSION BEYOND LIMITS OF REO 670-53-11-052. REMOVED RT 280.00 WEB. DUPLICATED WEB 0.040 7075T-6. LOCATE ALL HOLES EXCEPTING THOSE FROM RBL 42.50 OUTBOARD. DEBURR ALL ALODINE, PRIME TOPCOAT, IAW REO 670-53-11-052. DUPLICATED STRAPFeb 23, 2007 · N707EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR TRAX200700289Web · corrodedLEFT LOWER FS 280 WEB HAS CORROSION BEYOND LIMITS OF REO 670-53-11-052. REMOVED LT LOWER FS 280 WEB. REF STEPS OF FORM 412 FOR DUPLICATION OF WEB. OK TO INSTALL STRAP TO DOUBLER. INSTALLED 2 EA. LOWER ROWS OF FASTENERS W/ WET SOLID FASTENERS IAW CRJ SRM 51-4Feb 23, 2007 · N707EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR TRAX200700233Handle · crackedPAX DOOR OUTER HANDLE APPEARS TO BE CRACKED AT INNER AFT RADIUS (MARKED) REF: 52-830-102 PG 7, FIG 52-11-02 ATTACHED. PERFORMED LPI ON PANEL DOOR OUTER HANDLE INNER RADIUS VERIFIED CRACK IS PRESENT. IAW CRJ 700 NDT MANUAL 51-20-00-08. REPAIRED PER APPLICABLEFeb 15, 2007 · N707EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR TRAX200700202Light · inoperativeDURING PREFLIGHT INSPECTION, FOUND EXTERIOR EMERGENCY LIGHTS INOP/CREW RESET CB, NO HELP.Feb 9, 2007 · N707EV · Cndair CL6002C10 · Emergency LightingSDR TRAX200600705Step · brokenASD BOTTOM STEP BROKEN AT ATTACH LINK.Sep 5, 2006 · N707EV · Cndair CL6002B19 · Entrance StairsSDR ASOA05462Lamp · burned outDURING AN A-CHECK, THE EMERGENCY LIGHT AFT OF THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMPS IN THE EMERGENCY LIGHT AFT OF THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)May 25, 2005 · N707EV · Cndair CL6002C10 · Emergency LightingSDR ASOA05201Lamp · burned outFLT 4413 - DURING A GROUND INSPECTION IN SLC, THE EMERGENCY CEILING LIGHT AT ROWS 16 AND 17 WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE EMERGENCY CEILING LIGHT AT ROWS 16 AND 17. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 5, 2005 · N707EV · Cndair CL6002C10 · Emergency LightingSDR ASOA05150Step · brokenDURING A GROUND INSPECTION IN OKC, THE STRUT ON THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN OFF. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ASSEMBLY AND THE CONNECTING ROD SUPPORT ON THE PASSENGER DOOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (Feb 21, 2005 · N707EV · Cndair CL6002C10 · Entrance StairsSDR ASOA04337Lens · crackedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR.May 7, 2004 · N707EV · Cndair CL6002C10 · Emergency LightingSDR ASO2004F00013Lens · crackedDURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LENS AT THE SERVICE DOOR. (ASOA04337)May 7, 2004 · N707EV · Cndair CL6002C10 · Emergency LightingSDR ASOA04338Step · crackedDURING C-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP.Apr 30, 2004 · N707EV · Cndair CL6002C10 · Entrance StairsSDR ASOA03554Lamp · burned outDURING A GROUND INSPECTION IN DFW, THE EMERGENCY EXIT LIGHT BY THE SERVICE DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP BY THE SERVICE DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Nov 1, 2003 · N707EV · Cndair CL6002C10 · Emergency LightingSDR ASOA03464Control Unit · malfunctionedDURING CLIMB-OUT FROM OAK-DFW, THE CREW RECEIVED A SPLIT ELEVATOR CAUTION LIGHT. AN EMERGENCY WAS DECLARED WITH EMERGENCY VEHICLES REQUESTED FOR STAND BY AS A PRECAUTION. THE AIRCRAFT RETURNED TO OAK AND LANDED SAFELY. MAINTENANCE RESET THE ELEVATOR CONTROLSep 29, 2003 · N707EV · Cndair CL6002C10 · Elevator Control SystemSDR ASOA03390Fire Loop · malfunctionedDURING CLIMB-OUT FROM ATL-AGS, THE CREW RECEIVED A RIGHT BLEED DUCT WARNING MESSAGE. QRH WERE COMPLIED WITH AND AN EMERGENCY DECLARED. THE AIRCRAFT RETURNED TO ATL, LANDING SAFELY. MAINTENANCE READJUSTED THE LOOP ELEMENTS AT MT143 AND 144 AND MT204 AND 205 Aug 21, 2003 · N707EV · Cndair CL6002C10 · Fire DetectionSDR ASOA03121Door · stuckDURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND TO BE STUCK CLOSED. MAINTENANCE OPENED AND CLOSED THE PASSENGER DOOR SEVERAL TIMES BUT COULD NOT DUPLICATE THE PROBLEM. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)Mar 20, 2003 · N707EV · Cndair CL6002C10 · Passenger/Crew Doors
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